Pengendalian Sudut Pitch dan Roll Pesawat Flying Wing

The development of the aviation world in recent years has increased, one which is field unmanned aerial vehicles. This line with increasing use UAVs various fields, including for military missions, natural disaster monitoring and photography missions. Many types aircraft that can be used to complete these type widely flying wing aircraft. triangular shape does not have a tail. controller uses elevons on right left sides its wings, form relatively small, so this susceptible environmental disturbances causes flight mission failures. To overcome problem, control system needed able make maintain stability. In study, Linear Quadratic Regulator method was applied this. LQR pitch roll angles Based test results, interference given handled well by It proven when disturbance, experienced an overshoot 4.24º at angle 4.26º angle, but could quickly return setpoint within 1.2 seconds 1.3 angle. Thus